SERVICE TUBE FOR TURBINE ENGINE

• Main Authors: JAKOMIN JOHN MARTIN, RAJAGOPALAN VINODH, AGARA KARTHIK GOPAL RAO, FEMIA STEVEN PAUL
• Format: Patent
• Language: Chinese; English
• Published: 28.04.2020
• Subjects: AIR INTAKES FOR JET-PROPULSION PLANTS; BLASTING; COMBUSTION ENGINES; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS; GAS-TURBINE PLANTS; HEATING; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS; LIGHTING; MECHANICAL ENGINEERING; WEAPONS

An apparatus and method of reducing operating temperatures of a gas turbine engine (10), exposed to a service tube assembly (84) by utilizing a skirt (98) and radially outer mount (90). The reductionin temperature exposure minimizes temperatures of the service tube during engine operation to reduce...